A study of several theoretical methods for computing the zero-lift wave drag of a family of open-nosed bodies of revolution in the Mach number range of 2.0 to 4.0
Description:
Report presenting a computation of the wave drag of a family of open-nosed bodies of revolution was computed by six approximate theories: first-order perturbation theory, second-order perturbation theory, generalized shock-expansion theory, second-order shock-expansion theory, tangent-wedge theory, and impact theory. Results regarding the pressure distributions, wave drag, and computing time for each theory is provided.
Date:
September 1958
Creator:
Presley, Leroy L. & Mossman, Emmet A.
Item Type:
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Partner:
UNT Libraries Government Documents Department